IT8448432A0 - SYSTEM AND METHOD FOR INTENSIFYING THE THERMOENERGY CYCLE IN PROPULSION ENGINES BY MEANS OF AIR JET AND RELATED IMPROVED ENGINES - Google Patents

SYSTEM AND METHOD FOR INTENSIFYING THE THERMOENERGY CYCLE IN PROPULSION ENGINES BY MEANS OF AIR JET AND RELATED IMPROVED ENGINES

Info

Publication number
IT8448432A0
IT8448432A0 IT8448432A IT4843284A IT8448432A0 IT 8448432 A0 IT8448432 A0 IT 8448432A0 IT 8448432 A IT8448432 A IT 8448432A IT 4843284 A IT4843284 A IT 4843284A IT 8448432 A0 IT8448432 A0 IT 8448432A0
Authority
IT
Italy
Prior art keywords
engines
thermoenergy
intensifying
cycle
air jet
Prior art date
Application number
IT8448432A
Other languages
Italian (it)
Other versions
IT1177817B (en
Inventor
Paul A Marius
Original Assignee
Paul A Marius
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Paul A Marius filed Critical Paul A Marius
Publication of IT8448432A0 publication Critical patent/IT8448432A0/en
Application granted granted Critical
Publication of IT1177817B publication Critical patent/IT1177817B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Means For Warming Up And Starting Carburetors (AREA)
  • Control Of Turbines (AREA)
  • Percussion Or Vibration Massage (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
IT48432/84A 1983-06-20 1984-06-20 SYSTEM AND METHOD FOR INTENSIFYING THE THERMO-ENERGY CYCLE IN PROPULSION ENGINES BY AIR JET AND RELATED IMPROVED ENGINES IT1177817B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US50565883A 1983-06-20 1983-06-20

Publications (2)

Publication Number Publication Date
IT8448432A0 true IT8448432A0 (en) 1984-06-20
IT1177817B IT1177817B (en) 1987-08-26

Family

ID=24011258

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48432/84A IT1177817B (en) 1983-06-20 1984-06-20 SYSTEM AND METHOD FOR INTENSIFYING THE THERMO-ENERGY CYCLE IN PROPULSION ENGINES BY AIR JET AND RELATED IMPROVED ENGINES

Country Status (9)

Country Link
EP (1) EP0146624B1 (en)
JP (1) JPS60501616A (en)
AU (1) AU3210384A (en)
BR (1) BR8406943A (en)
CA (1) CA1235583A (en)
DE (1) DE3477229D1 (en)
DK (1) DK77385D0 (en)
IT (1) IT1177817B (en)
WO (1) WO1985000199A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4858428A (en) * 1986-04-24 1989-08-22 Paul Marius A Advanced integrated propulsion system with total optimized cycle for gas turbines
US4916896A (en) * 1988-11-02 1990-04-17 Paul Marius A Multiple propulsion with quatro vectorial direction system
FR2670869B1 (en) * 1990-12-19 1994-10-21 Snecma COMBUSTION CHAMBER COMPRISING TWO SUCCESSIVE SPEAKERS.
JP2988109B2 (en) * 1991-03-20 1999-12-06 株式会社日立製作所 Rotor shaft for rotating electric machine and rotating electric machine using the same
GB9418949D0 (en) * 1994-09-20 1994-11-09 Helliwell Brian J 90% thermal efficient gas turbine engine
DE19902437C5 (en) * 1999-01-22 2017-01-12 General Electric Technology Gmbh Method and device for rapid startup and for rapid increase in output of a gas turbine plant
EP2622192A2 (en) * 2010-09-30 2013-08-07 General Electric Company Aircraft engine systems and methods for operating same
WO2012173651A1 (en) * 2011-06-17 2012-12-20 General Electric Company Aircraft engine fuel system and method of operating the same
US9709069B2 (en) 2013-10-22 2017-07-18 Dayspring Church Of God Apostolic Hybrid drive engine
JP7250304B2 (en) * 2018-09-26 2023-04-03 国立大学法人室蘭工業大学 Propellant for gas generator for turbine drive and method for producing the same

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2360130A (en) * 1941-03-26 1944-10-10 Armstrong Siddeley Motors Ltd High-speed propulsion plant
US2416389A (en) * 1942-06-17 1947-02-25 Armstrong Siddeley Motors Ltd Torque balancing of jet propulsion turbine plant
FR924012A (en) * 1946-02-18 1947-07-24 Const Aeronautiques Du Ct Soc Further development of combustion turbines
US2647368A (en) * 1949-05-09 1953-08-04 Hermann Oestrich Method and apparatus for internally cooling gas turbine blades with air, fuel, and water
DE846341C (en) * 1950-06-20 1952-08-11 Gustav Fillon Blading with internal cooling for gas turbines with combustion within the blade channels
CH308992A (en) * 1951-05-16 1955-08-15 Power Jets Res & Dev Ltd Gas turbine plant.
US2970807A (en) * 1957-05-28 1961-02-07 Messerschmitt Ag Rotor blades for gas turbines
US3747339A (en) * 1961-11-13 1973-07-24 Texaco Inc Reaction propulsion engine and method of operation
DE1231959B (en) * 1963-06-28 1967-01-05 M A N Turbo G M B H As a twin-flow engine in single-shaft design, lift jet engine for aircraft
GB1039677A (en) * 1963-07-10 1966-08-17 Rolls Royce Combustion chamber for a gas turbine engine
US3740949A (en) * 1963-11-20 1973-06-26 Texaco Inc Fuel cooled ram air reaction propulsion engine
DE1261357B (en) * 1965-12-14 1968-02-15 Dornier Gmbh Gas turbine engine
US3486340A (en) * 1967-05-05 1969-12-30 Garrett Corp Gas turbine powerplant with means for cooling compressed air
US3600890A (en) * 1968-11-29 1971-08-24 United Aircraft Corp Turbine cooling construction
CH573571A5 (en) * 1974-01-11 1976-03-15 Sulzer Ag
US4054030A (en) * 1976-04-29 1977-10-18 General Motors Corporation Variable cycle gas turbine engine
US4118145A (en) * 1977-03-02 1978-10-03 Westinghouse Electric Corp. Water-cooled turbine blade
US4190398A (en) * 1977-06-03 1980-02-26 General Electric Company Gas turbine engine and means for cooling same
US4242045A (en) * 1979-06-01 1980-12-30 General Electric Company Trap seal for open circuit liquid cooled turbines

Also Published As

Publication number Publication date
DK77385A (en) 1985-02-20
EP0146624B1 (en) 1989-03-15
DK77385D0 (en) 1985-02-20
JPS60501616A (en) 1985-09-26
WO1985000199A1 (en) 1985-01-17
DE3477229D1 (en) 1989-04-20
CA1235583A (en) 1988-04-26
BR8406943A (en) 1985-06-04
EP0146624A4 (en) 1986-03-18
EP0146624A1 (en) 1985-07-03
IT1177817B (en) 1987-08-26
AU3210384A (en) 1985-01-25

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19921230